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GB2277305B - Mechanism for moving flap - Google Patents

Mechanism for moving flap

Info

Publication number
GB2277305B
GB2277305B GB9408028A GB9408028A GB2277305B GB 2277305 B GB2277305 B GB 2277305B GB 9408028 A GB9408028 A GB 9408028A GB 9408028 A GB9408028 A GB 9408028A GB 2277305 B GB2277305 B GB 2277305B
Authority
GB
United Kingdom
Prior art keywords
moving flap
flap
moving
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
GB9408028A
Other versions
GB2277305A (en
GB9408028D0 (en
Inventor
Graham James Walden
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by British Aerospace PLC filed Critical British Aerospace PLC
Publication of GB9408028D0 publication Critical patent/GB9408028D0/en
Publication of GB2277305A publication Critical patent/GB2277305A/en
Application granted granted Critical
Publication of GB2277305B publication Critical patent/GB2277305B/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Transmission Devices (AREA)
GB9408028A 1993-04-22 1994-04-22 Mechanism for moving flap Expired - Lifetime GB2277305B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB939308336A GB9308336D0 (en) 1993-04-22 1993-04-22 Mechanism for moving flap

Publications (3)

Publication Number Publication Date
GB9408028D0 GB9408028D0 (en) 1994-06-15
GB2277305A GB2277305A (en) 1994-10-26
GB2277305B true GB2277305B (en) 1997-01-22

Family

ID=10734286

Family Applications (2)

Application Number Title Priority Date Filing Date
GB939308336A Pending GB9308336D0 (en) 1993-04-22 1993-04-22 Mechanism for moving flap
GB9408028A Expired - Lifetime GB2277305B (en) 1993-04-22 1994-04-22 Mechanism for moving flap

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GB939308336A Pending GB9308336D0 (en) 1993-04-22 1993-04-22 Mechanism for moving flap

Country Status (1)

Country Link
GB (2) GB9308336D0 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006030315A1 (en) * 2006-06-30 2008-01-17 Airbus Deutschland Gmbh High-lift system on the wing of an aircraft
DE102011018906A1 (en) * 2011-04-28 2012-10-31 Airbus Operations Gmbh High lift system for an aircraft and method for influencing the high lift characteristics of an aircraft
EP2886451A1 (en) * 2013-12-18 2015-06-24 Airbus Operations GmbH Trailing-edge flap system for a wing of an aircraft and aircraft comprising a wing and at least one such trailing-edge flap system
FR3058983B1 (en) * 2016-11-22 2018-11-02 Safran Electronics & Defense EASILY MOUNTED ACTUATOR
US10974816B2 (en) 2017-09-28 2021-04-13 The Boeing Company High-fowler flap actuation apparatus and related methods

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB941904A (en) * 1960-12-27 1963-11-13 Ludwig Bolkow Improvements relating to aircraft having hinged wings, flaps, fins or like parts with control surfaces
EP0045987A1 (en) * 1980-08-13 1982-02-17 The Boeing Company Extendible airfoil cable drum track assembly

Also Published As

Publication number Publication date
GB9308336D0 (en) 1993-06-09
GB2277305A (en) 1994-10-26
GB9408028D0 (en) 1994-06-15

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Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
PE20 Patent expired after termination of 20 years

Expiry date: 20140421